2007 ICCM-16 Kyoto Japan
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ICCM-16 Sixteenth International Conference on Composite Materials

July/11 (Wed.) -- Room J

July -- 8(Sun.) / 9(Mon.) / 10(Tue.) / 11(Wed.) / 12(Thr.) / 13(Fri.)

July/11(Wed.) -- Room A / B-2 / F / G / H / I / J / K / Poster Session (B-1)

Wednesday Morning (July 11) -- Room J: 9:20-13:20
Session Title: Simulation and Design of Aircraft Composite Structures
Presenters Name Affiliation Country Paper Title pdf
Chairperson(s): Kwang Soo Kim
Emilio V. Gonzalez Universitat de Girona, Spain Composite skin-stiffener virtual testing WeJM1-01
Pere Maimi Universitat de Girona Spain
Albert Turon Universitat de Girona Spain
Pedro P. Camanho Universidade do Porto Portugal
Joan-Andreu Mayugo Universitat de Girona Spain
Go Matsubara KAWASAKI HEAVY INDUSTRIES,LTD. Japan FAILURE STRENGTH PREDICTION FOR CFRP STIFFENED PANEL WeJM1-02
Fumihide Inamura KAWASAKI HEAVY INDUSTRIES,LTD. Japan
Hirokazu Matsuda KAWASAKI HEAVY INDUSTRIES,LTD. Japan
Soo-Hyun Kim Korea Advanced Institute of Science and Technology Korea Postbuckling Analysis and Optimization of Composite Stiffened Panel Considering Skin-Stiffener Debonding WeJM1-03
Chun-Gon Kim Korea Advanced Institute of Science and Technology Korea
Chun Li National Research Council Canada Canada Investigation of an Accelerated Moisture Removal Approach of a Composite Aircraft Control Surface WeJM1-04
Rick Ueno Univeristy of Ottawa Canada
Vivier Lefebve Department of National Defence Canada Canada
Kwang Soo Kim Korea Aerospace Research Institute Korea Experimental Study of Composite Bonded Skin-Stiffener Specimens WeJM1-05
Jae Mo An Korea Aerospace Research Institute Korea
Young Soon Jang Korea Aerospace Research Institute Korea
Yeong Moo Yi Korea Aerospace Research Institute Korea
Mengchun Yu National Cheng Kung University Taiwan AEROELASTIC DIVERGENCE AND FREE VIBRATION OF TAPERED COMPOSITE WINGS WeJM1-06
Chyanbin Hwu National Cheng Kung University Taiwan
In-Gyu Lim Korea Advanced Institute of Science and Technology Korea AEROELASTIC ANALYSIS OF BEARINGLESS ROTORS WITH COMPOSITE FLEXBEAM IN HOVER AND FORWARD FLIGHT WeJM1-07
In Lee Korea Advanced Institute of Science and Technology Korea
In Seong Hwang Seoul National University Korea STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES WeJM1-08
Seung Yong Min Seoul National University Korea
Choong Hee Lee Seoul National University Korea
Seung Jo Kim Seoul National University Korea
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Wednesday Afternoon (July 11) -- Room J: 13:20-(18:00)
Session Title: Simulation and Design of Aircraft Composite Structures
Name Affiliation Country Paper Title pdf
Chairperson(s): Yosuke Nagao
Markus Kaufmann Kungliga Tekniska Högskolan (KTH) Sweden Integrated cost/weight optimization of composite skin/stringer elements WeJA1-01
Dan Zenkert Kungliga Tekniska Högskolan (KTH) Sweden
Per Wennhage Kungliga Tekniska Högskolan (KTH) Sweden
Juil Kim Chosun Univesity Korea A STUDY ON CONCEPTUAL STRUCTURAL DESIGN OF FUSELAGE FOR A SMALL SCALE WIG VEHICLE USING COMPOSITE MATERIALS WeJA1-02
Chang-Duk Kong Chosun Univesity Korea
Seounghyeon Lee Chosun Univesity Korea
Yoshihiko Sugiyama Rykoku University Japan
Chang-Duk Kong Chosun University Korea STRUCTURAL DESIGN ON WING OF A SMALL SCALE WIG VEHICLE WITH CARBON/EPOXY AND FOAM SANDWICH COMPOSITE STRUCTURE WeJA1-03
Hyunbum Park Chosun University Korea
Younggwang Kim Chosun University Korea
Kukjin Kang Korea Ocean Research & Development Institute Korea
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